Application of pseudo-cooling boundary conditions combined with electromagnetic and thermal weak coupling for the analysis of highly integrated aerospace actuators

T. D. Kefalas, A. Kladas
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Abstract

Two original numerical techniques are presented for the finite-element (FE) unsteady analysis of permanent magnet synchronous motors (PMSM) and induction motors (IM) operating in demanding aerospace applications. The first technique is the electromagnetic and thermal analysis weak coupling using a multi-slice FE model. The advantage of this technique is the representation of complex actuator geometries including skewed magnets, by using a low computational cost 2-D model while taking into consideration temperature dependent material attributes. The second technique deals with the application of pseudo-cooling boundary conditions for the emulation of the cooling housing of actuators. Those boundary conditions are applied at the outer areas of the actuators in contact with the housing and eliminate the need of modeling complex 3-D geometries of highly integrated actuator housings.
结合电磁和热弱耦合的伪冷却边界条件在高集成航空航天作动器分析中的应用
提出了两种新颖的数值分析方法,用于在苛刻的航天应用中运行的永磁同步电动机和感应电动机的有限元非定常分析。第一种技术是利用多层有限元模型进行电磁和热弱耦合分析。该技术的优点是,通过使用低计算成本的二维模型,同时考虑到与温度相关的材料属性,可以表示包括偏斜磁铁在内的复杂驱动器几何形状。第二种技术处理伪冷却边界条件在执行器冷却壳仿真中的应用。这些边界条件应用于执行器与壳体接触的外部区域,消除了对高度集成的执行器壳体复杂三维几何形状建模的需要。
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